FSC 1560 Airframe Structural Components: 1560-00-250-7073, 1560-00-250-7399, 1560-00-250-7400
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 1560-00-250-7073 1560002507073 | 265-530292-17 | Panel, Structural, Aircraft | Boeing Company, The (43999) | ||
| 1560-00-250-7074 1560002507074 | 265-530292-39 | Panel, Structural, Aircraft | Boeing Company, The (43999) | ||
| 1560-00-250-7077 1560002507077 | 265-530292-23 | Panel, Structural, Aircraft | Boeing Company, The (43999) | ||
| 1560-00-250-7081 1560002507081 | 12W9274-10 | Bracket, Structural Component, Air | Aircraft Mission Design Series: F-111 Aircraft Location: Actuator flap track bracket Overall Length: 2.170 inches nominal | Lockheed Martin Corporation (81755) | |
| 1560-00-250-7082 1560002507082 | 12W9274-9 | Bracket, Structural Component, Air | Aircraft Mission Design Series: F-111 Aircraft Location: Vane actuation flap bracket pin Overall Length: 2.170 inches nominal | Lockheed Martin Corporation (81755) | |
| 1560-00-250-7085 1560002507085 | 12W9282-14 12W9282-10 | Guide, Actuation Lever | General Characteristics Item Description: Steel, AMS5355, 2.560 in. lg, 0.213 in. min, 0.221 in. max W, elongated hole thru 2 places | Lockheed Martin Corporation (81755) | |
| 1560-00-250-7086 1560002507086 | 12W9282-13 12W9282-9 | Guide, Actuation Lever | General Characteristics Item Description: Steel, AMS5355, 2.560 in. lg, 0.213 in. min, 0.221 in. max W, elongated hole thru 2 places | Lockheed Martin Corporation (81755) | |
| 1560-00-250-7092 1560002507092 | 265-321200-127 | Plate, Structural, Aircraft | III End Item Identification: T-39 trainer airplane. Aircraft Mission Design Series: T-39 Material: Aluminum alloy 2024 | Sabreliner Corporation (0ESK8) Boeing Company, The (43999) | |
| 1560-00-250-7093 1560002507093 | 265-321200-143 | Plate, Structural, Aircraft | III End Item Identification: C-5 galaxy airplane. Aircraft Mission Design Series: C-5A Material: Steel comp 321 | Boeing Company, The (43999) | |
| 1560-00-250-7095 1560002507095 | 265-321200-161 | Doubler, Nacelle Nos | Boeing Company, The (43999) | ||
| 1560-00-250-7096 1560002507096 | 265-321200-159 | Angle, Nacelle Nose | General Characteristics Item Description: Aluminum alloy, QQ-A-250/5 | Boeing Company, The (43999) | |
| 1560-00-250-7101 1560002507101 | 265-321200-167 | Filler, Nacelle Nose | III End Item Identification: Aircraft model T39 | Boeing Company, The (43999) | |
| 1560-00-250-7102 1560002507102 | 265-321200-169 | Filler, Nacelle Nose | III End Item Identification: Aircraft model T39 | Boeing Company, The (43999) | |
| 1560-00-250-7104 1560002507104 | 1050-530338-51 | Partition, Oxygen Cylinder | Boeing Company, The (43999) | ||
| 1560-00-250-7105 1560002507105 | 1050-530338-21 | Partition, Oxygen Cylinder | Boeing Company, The (43999) | ||
| 1560-00-250-7372 1560002507372 | 60742 60742-00 | Panel, Tail Inspecti | Piper Aircraft Inc. (77294) | ||
| 1560-00-250-7373 1560002507373 | 60742-01 60742-1 | Panel, Tail Inspecti | Piper Aircraft Inc. (77294) | ||
| 1560-00-250-7397 1560002507397 | 3P21851-104 | Flange, Bifurcated Duct | III End Item Identification: Aircraft model C141 | Lockheed Martin Corporation (98897) | |
| 1560-00-250-7399 1560002507399 | 3W22000-125 | Skin, Aircraft | Aircraft Mission Design Series: C-141 | Lockheed Martin Corporation (98897) | |
| 1560-00-250-7400 1560002507400 | 3T21004-101 | Cover, Hinge, Rudder | General Characteristics Item Description: Aluminum alloy 2024 T3 QQ-A-250-5 | Lockheed Martin Corporation (98897) |